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Results: 1 through 50 of 185 (1.055 secs)
You searched for: subject:"Aerodynamics--Research."
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[texts]Theory of propellers.: II,Method for calculating the axial interference velocity - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807489&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 153
[texts]Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854698&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 88
[texts]Column and plate compressive strengths of aircraft structural materials 24S-T aluminum-alloy sheet - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804757&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 147
[texts]NACA impact basin and water landing tests of a float model at various velocities and weights - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804832&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 134
[texts]Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614294&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 144
[texts]Analysis of vertical-tail loads in rolling pull-out maneuvers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806701&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 111
[texts]Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854699&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 64
[texts]Effects of Reynolds number and leading-edge roughness on lift and drag characteristics of the NACA 653-418, a = 1.0 airfoil section - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638084&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerodynamics--Research
Downloads: 163
[texts]Climb and high-speed tests of a Curtiss no. 714-1C2-12 four-blade propeller on the Republic P-47C airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807441&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 122
[texts]Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616345&ix=nu&I=0&V=D&pm=1
Keywords: Parachutes; Aerodynamics--Research
Downloads: 166
[texts]Some measurements of time and space correlation in wind tunnel - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807829&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 107
[texts]Frequency of occurrence of atmospheric gusts and of related loads on airplane structures - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808565&ix=nu&I=0&V=D&pm=1
Keywords: Airframes; Aerodynamics--Research
Downloads: 90
[texts]Exploratory investigation of transpiration cooling of a 40° double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295° to 2,910° F - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853034&ix=nu&I=0&V=D&pm=1
Keywords: Transpiration (Physics; Aerodynamics--Research
Downloads: 58
[texts]Flight tests of the lateral control characteristics of an F6F-3 airplane equipped with spring-tab ailerons - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605252&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 105
[texts]Some notes on the determination of the stick-free neutral point from wind-tunnel data - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804989&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 110
[texts]Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805102&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 101
[texts]Wind-tunnel tests of dual-rotating propellers with systematic differences in number of blades, blade setting, and rotational speed of front and rear propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638089&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 124
[texts]Method for studying the hunting oscillations of an airplane with a simple type of automatic control - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614297&ix=nu&I=0&V=D&pm=1
Keywords: Oscillations; Aerodynamics--Research
Downloads: 85
[texts]Supersaturation in the spontaneous formation of nuclei in water vapor - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807868&ix=nu&I=0&V=D&pm=1
Keywords: Condensation--Research; Aerodynamics--Research
Downloads: 80
[texts]Effect of compressibility on the pressures and forces acting on a modified NACA 65,3-019 airfoil having a 0.20-chord flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638549&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Compressibility; Aerodynamics--Research
Downloads: 121
[texts]Effect of powered propellers on the aerodynamic characteristics and the porpoising stability of a dynamic model of a long-range flying boat - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805116&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 89
[texts]Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807484&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 112
[texts]Kinetic treatment of the nucleation in supersaturated vapors - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807766&ix=nu&I=0&V=D&pm=1
Keywords: Atmospheric nucleation; Aerodynamics--Research
Downloads: 93
[texts]Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804830&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 134
[texts]Effects of heat-capacity lag in gas dynamics - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614317&ix=nu&I=0&V=D&pm=1
Keywords: Carbon dioxide; Aerodynamics--Research
Downloads: 114
[texts]Charts of pressure, density, and temperature changes at an abrupt increase in cross-sectional area of flow of compressible air - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003619235&ix=nu&I=0&V=D&pm=1
Keywords: Thermodynamic cycles; Aerodynamics--Research
Downloads: 105
[texts]Theories of turbulence - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807732&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence; Aerodynamics--Research
Downloads: 162
[texts]Effects on low-speed spray characteristics of various modifications to a powered model of the Boeing XPBB-1 flying boat - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804846&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 104
[texts]Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Drag (Aerodynamics
Downloads: 191
[texts]Determination of effective column length from strain measurements - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804669&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 120
[texts]Approximate determination of the power required to move control surfaces as related to control-booster design - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614183&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 102
[texts]Force tests of a 1/5-scale model of the type GB-5 controllable glide bomb - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003610203&ix=nu&I=0&V=D&pm=1
Keywords: Guided bombs; Aerodynamics--Research
Downloads: 126
[texts]Maximum rates of control motion obtained from ground tests - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613620&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 57
[texts]Column and plate compressive strengths of aircraft structural materials extruded 75S-T aluminum-alloy - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807482&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 121
[texts]Theory of propellers.:I, Determination of the circulation function and the mass coefficient for dual-rotating propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003622107&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 142
[texts]Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 652-415, 653-418 and 654-421 airfoil sections - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806709&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 188
[texts]Note on compressibility effects on downwash at the tail at subcritical speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003617581&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 133
[texts]Charts for determining propeller efficiency - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614447&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 147
[texts]Resistance tests of models of three flying-boat hulls with a length-beam ration of 10.5 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638098&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Nacelles; Aerodynamics--Research
Downloads: 129
[texts]Determination of the stability and control characteristics of a tailless all-wing airplane model with sweepback in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616137&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 119
[texts]Effect of initial displacement of the center support on the buckling of a column continuous over three supports - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804949&ix=nu&I=0&V=D&pm=1
Keywords: Buckling (Mechanics; Aerodynamics--Research
Downloads: 126
[texts]Aerodynamic tests of an M-31 bomb in the 8-foot high-speed tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003612647&ix=nu&I=0&V=D&pm=1
Keywords: Projectiles, Aerial; Aerodynamics--Research
Downloads: 78
[texts]Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806635&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 135
[texts]Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616157&ix=nu&I=0&V=D&pm=1
Keywords: Wakes (Aerodynamics; Aerodynamics--Research
Downloads: 141
[texts]Experimental pressure distributions over two wing-body combinations at Mach number 1.9 - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810661&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Aerodynamics--Research
Downloads: 71
[texts]Simple method for estimating terminal velocity including effect of compressibility on drag - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638273&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 95
[texts]Effect of compressibility on the hovering performance of two 10-foot-diameter helicopter rotors tested in the Langley full-scale tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834396&ix=nu&I=0&V=D&pm=1
Keywords: Rotors (Helicopters; Aerodynamics--Research
Downloads: 115
[texts]Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808495&ix=nu&I=0&V=D&pm=1
Keywords: Afterburners--Research; Aerodynamics--Research
Downloads: 77
[texts]Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806616&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 131
[texts]Tests of a linked differential flap system designed to minimize the reduction in effective dihedral caused by power - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003631486&ix=nu&I=0&V=D&pm=1
Keywords: Flaps (Airplanes; Aerodynamics--Research
Downloads: 90
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